Ablation and thermal response program for spacecraft heatshield analysis

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Chen, Y K ^a   Milos, Frank S ^a  

^a NASA AMES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; CODES (SYMBOLS); NASA; SPACE FLIGHT; THERMOANALYSIS;

AMES RESEARCH CENTERS; CHARRING MATERIALS; GOVERNING EQUATIONS; ISOTROPIC MATERIALS; LIGHT-WEIGHT CERAMICS; NUMERICAL EXPERIMENTS; NUMERICAL PROCEDURES; THERMAL ENERGY TRANSPORT;

ABLATION;

EID: 84982317965     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (22)

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2. Anon., User's Manual: Aerotherm Charring Material Thermal Response and Ablation Program, Acurex Corporation, Aerotherm Division, Mountain View, California, Aug. 1987.
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4. Olynick, D. R., Chen, Y.-K., and Tauber, M. E. "Forebody TPS Sizing with Radiation and Ablation for the Stardust Sample Return Capsule," AIAA Paper 972474, June 1997.
5. Chen, Y.-K., and Milos, F. S., "Fully Implicit Ablation and Thermal Analysis Program (FIAT)," ICCE/4, Proc. Fourth International Conference on Composites Engineering, ICCE and College of Engineering, University of New Orleans, July 1997, pp. 661-662.
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8. Tran, H., Private Communication, Thermal Protection Materials and Systems Branch, NASA Ames Research Center, March 1996.
9. Stardust Aerothermal & Materials Working Group Meeting, Space Directorate, NASA Ames Research Center, Feb. 8, 1996.
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11. Mitcheltree, R. A., Private Communication, Aerothermodynamics Branch, NASA Langley Research Center, June 1996.
12. Tauber, M. E., Wercinski, P. F., Papadopoulos, P., Yang, L., and Paterson, J., "Estimates of Heatshielding Requirements for Saturn Probe Missions," Final Report submitted to Dr. L. Lasher, Space Projects Division, in support of the Outer Planet Mission Studies Task, July 29, 1994.
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16. Milos, F. S., Chen, Y.-K., and Henline, W. D., "Methodology for Full-Body TPS Sizing of Access-to-Space Vehicles," AIAA Paper 96-0614, Jan. 1996.
17. Milos, F. S., and Chen, Y.-K., "Comprehensive Model for Multi-Component Ablation Thermochemistry," AIAA Paper 97-0141, Jan. 1997.
18. Squire, T. H., Milos, F. S., Hartlieb, G. C., and Rasky, D. J., "TPSX: Thermal Protection Systems Expert and Material Properties," ICCE/4, Proc. Fourth International Conference on Composites Engineering, ICCE and College of Engineering, University of New Orleans, July 1997, pp. 937-938.
19. Chen, Y.-K., and Milos, F. S., "Solution Strategy for Thermal Response of Non-Ablating Thermal Protection System Materials at Hypersonic Speeds," AIAA Paper 960615, Jan. 1996.
20. Chen, Y.-K., Henline, W. D., Stewart, D. A., and Candler, G. V., "Navier-Stokes Solutions with Surface Catalysis for Martian Atmospheric Entry," Journal of Spacecraft and Rockets, Vol. 30, No. 1, 1993, pp. 32-42.
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